Gyrostat dynamics on a circular orbit

Publication

dc.contributor.advisor	Silva, André Resende Rodrigues da
dc.contributor.author	Santos, Luís Filipe Ferreira Marques
dc.date.accessioned	2014-07-16T09:54:44Z
dc.date.available	2014-07-16T09:54:44Z
dc.date.issued	2009
dc.description.abstract	This work deals with a general gyrostat moving along a circular orbit in a central Newtonian force field. The main purpose is to determine all equilibria positions for our spacecraft in the case when internal angular momentum of the gyrostat satellite is collinear to its principal axis of inertia, when the gyrostatic moment vector lies in one of the satellite’s principal central plane of inertia and for a general position where the gyrostatic moment doesn’t coincide with any of the principal axis of inertia.	por
dc.identifier.uri	http://hdl.handle.net/10400.6/2045
dc.language.iso	eng	por
dc.peerreviewed	yes	por
dc.publisher	Universidade da Beira Interior	por
dc.subject	Veículo espacial	por
dc.subject	Dinâmica girostática	por
dc.title	Gyrostat dynamics on a circular orbit	por
dc.type	master thesis
dspace.entity.type	Publication
oaire.citation.conferencePlace	Covilhã	por
person.familyName	Santos
person.givenName	Luis
person.identifier.ciencia-id	6717-B0D3-0F5B
person.identifier.orcid	0000-0002-7169-2660
person.identifier.rid	I-6614-2015
person.identifier.scopus-author-id	12768907700
rcaap.rights	openAccess	por
rcaap.type	masterThesis	por
relation.isAuthorOfPublication	58ad442e-76b5-4fe4-8cc4-0456573e5709
relation.isAuthorOfPublication.latestForDiscovery	58ad442e-76b5-4fe4-8cc4-0456573e5709

Files

Now showing 1 - 1 of 1

Now showing 1 - 1 of 1